ATE524576T1 - METHOD FOR PRODUCING AN ABRASIVE COATING ON A GAS TURBINE COMPONENT - Google Patents

METHOD FOR PRODUCING AN ABRASIVE COATING ON A GAS TURBINE COMPONENT

Info

Publication number
ATE524576T1
ATE524576T1 AT07789521T AT07789521T ATE524576T1 AT E524576 T1 ATE524576 T1 AT E524576T1 AT 07789521 T AT07789521 T AT 07789521T AT 07789521 T AT07789521 T AT 07789521T AT E524576 T1 ATE524576 T1 AT E524576T1
Authority
AT
Austria
Prior art keywords
gas turbine
alloy powder
turbine component
melting alloy
temperature melting
Prior art date
Application number
AT07789521T
Other languages
German (de)
Inventor
Karl-Heinz Manier
Ilya Chuprakov
Robert Sparling
Original Assignee
Mtu Aero Engines Gmbh
Liburdi Engineering
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mtu Aero Engines Gmbh, Liburdi Engineering filed Critical Mtu Aero Engines Gmbh
Application granted granted Critical
Publication of ATE524576T1 publication Critical patent/ATE524576T1/en

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C30/00—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C24/00—Coating starting from inorganic powder
    • C23C24/08—Coating starting from inorganic powder by application of heat or pressure and heat
    • C23C24/10—Coating starting from inorganic powder by application of heat or pressure and heat with intermediate formation of a liquid phase in the layer
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288—Protective coatings for blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/30—Manufacture with deposition of material
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/40—Heat treatment
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/20—Oxide or non-oxide ceramics
    • F05D2300/22—Non-oxide ceramics
    • F05D2300/228—Nitrides
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/20—Oxide or non-oxide ceramics
    • F05D2300/22—Non-oxide ceramics
    • F05D2300/228—Nitrides
    • F05D2300/2283—Nitrides of silicon

Abstract

A method for manufacturing an abrasive coating on a gas turbine component, especially on a gas turbine rotor blade tip, comprising at least the following steps: a) providing a gas turbine component, especially a gas turbine rotor blade; b) providing a high temperature melting alloy powder; c) providing abrasive particles; d) providing a low temperature melting alloy powder; e) blending at least said high temperature melting alloy powder and said abrasive particles to provide a mixture; f) applying said low temperature melting alloy powder and said mixture to an area of said gas turbine component, especially to a tip of said turbine rotor blade; g) locally heating said area of said gas turbine component to a temperature above the melting point of said low temperature melting alloy powder but below the melting point of said high temperature melting alloy powder is provided.
AT07789521T 2007-05-04 2007-05-04 METHOD FOR PRODUCING AN ABRASIVE COATING ON A GAS TURBINE COMPONENT ATE524576T1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/IB2007/002079 WO2008135803A1 (en) 2007-05-04 2007-05-04 Method for manufacturing an abrasive coating on a gas turbine component

Publications (1)

Publication Number Publication Date
ATE524576T1 true ATE524576T1 (en) 2011-09-15

Family

ID=38649958

Family Applications (1)

Application Number Title Priority Date Filing Date
AT07789521T ATE524576T1 (en) 2007-05-04 2007-05-04 METHOD FOR PRODUCING AN ABRASIVE COATING ON A GAS TURBINE COMPONENT

Country Status (7)

Country Link
US (1) US9322100B2 (en)
EP (1) EP2171124B1 (en)
JP (1) JP4910096B2 (en)
KR (1) KR101372342B1 (en)
AT (1) ATE524576T1 (en)
CA (1) CA2679517C (en)
WO (1) WO2008135803A1 (en)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008003100A1 (en) * 2008-01-03 2009-07-16 Mtu Aero Engines Gmbh Solder coating, method for coating a component, component and adhesive tape with a solder coating
DE102009031313B4 (en) 2009-06-30 2018-07-05 MTU Aero Engines AG Coating and method for coating a component
US9169740B2 (en) * 2010-10-25 2015-10-27 United Technologies Corporation Friable ceramic rotor shaft abrasive coating
DE102011086524A1 (en) 2011-11-17 2013-05-23 Mtu Aero Engines Gmbh Armouring of sealing fins of TiAl blades by inductive soldering of hard material particles
US9598973B2 (en) * 2012-11-28 2017-03-21 General Electric Company Seal systems for use in turbomachines and methods of fabricating the same
US9926794B2 (en) 2013-03-15 2018-03-27 United Technologies Corporation Turbine blade tip treatment for industrial gas turbines
US9849533B2 (en) 2013-05-30 2017-12-26 General Electric Company Hybrid diffusion-brazing process and hybrid diffusion-brazed article
US10786875B2 (en) * 2014-07-02 2020-09-29 Raytheon Technologies Corporation Abrasive preforms and manufacture and use methods
US10018056B2 (en) * 2014-07-02 2018-07-10 United Technologies Corporation Abrasive coating and manufacture and use methods
US10012095B2 (en) * 2014-07-02 2018-07-03 United Technologies Corporation Abrasive coating and manufacture and use methods
US10030527B2 (en) * 2014-07-02 2018-07-24 United Technologies Corporation Abrasive preforms and manufacture and use methods
DE102016206558A1 (en) 2016-04-19 2017-10-19 MTU Aero Engines AG Method and device for producing at least one component region of a component
US10512989B2 (en) * 2017-02-21 2019-12-24 General Electric Company Weld filler metal
DE102019202926A1 (en) 2019-03-05 2020-09-10 Siemens Aktiengesellschaft Two-layer abrasive layer for blade tip, process component and turbine arrangement
IT201900003691A1 (en) * 2019-03-13 2020-09-13 Nuovo Pignone Tecnologie Srl Abrasive terminal of a rotor blade for a turboexpander
DE102019207350A1 (en) * 2019-05-20 2020-11-26 Siemens Aktiengesellschaft Welding process with coated abrasive particles, coated abrasive particles, layer system and sealing system
US11612986B2 (en) 2019-12-17 2023-03-28 Rolls-Royce Corporation Abrasive coating including metal matrix and ceramic particles

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4257741A (en) * 1978-11-02 1981-03-24 General Electric Company Turbine engine blade with airfoil projection
CA1202768A (en) * 1981-11-05 1986-04-08 Kenneth R. Cross Method for forming braze-bonded abrasive turbine blade tip
US4610698A (en) 1984-06-25 1986-09-09 United Technologies Corporation Abrasive surface coating process for superalloys
US4735656A (en) * 1986-12-29 1988-04-05 United Technologies Corporation Abrasive material, especially for turbine blade tips
US4851188A (en) * 1987-12-21 1989-07-25 United Technologies Corporation Method for making a turbine blade having a wear resistant layer sintered to the blade tip surface
CA2048804A1 (en) * 1990-11-01 1992-05-02 Roger J. Perkins Long life abrasive turbine blade tips
US5453329A (en) * 1992-06-08 1995-09-26 Quantum Laser Corporation Method for laser cladding thermally insulated abrasive particles to a substrate, and clad substrate formed thereby
US5359770A (en) 1992-09-08 1994-11-01 General Motors Corporation Method for bonding abrasive blade tips to the tip of a gas turbine blade
DE4439950C2 (en) 1994-11-09 2001-03-01 Mtu Muenchen Gmbh Metallic component with a composite coating, use, and method for producing metallic components
US5655701A (en) * 1995-07-10 1997-08-12 United Technologies Corporation Method for repairing an abradable seal
US6355086B2 (en) 1997-08-12 2002-03-12 Rolls-Royce Corporation Method and apparatus for making components by direct laser processing
US5935407A (en) 1997-11-06 1999-08-10 Chromalloy Gas Turbine Corporation Method for producing abrasive tips for gas turbine blades
US6451454B1 (en) * 1999-06-29 2002-09-17 General Electric Company Turbine engine component having wear coating and method for coating a turbine engine component
US20040124231A1 (en) * 1999-06-29 2004-07-01 Hasz Wayne Charles Method for coating a substrate
JP3801452B2 (en) 2001-02-28 2006-07-26 三菱重工業株式会社 Abrasion resistant coating and its construction method
JP3902179B2 (en) * 2001-05-31 2007-04-04 三菱重工業株式会社 Film forming method, film forming material, and abrasive film forming sheet
US6706319B2 (en) 2001-12-05 2004-03-16 Siemens Westinghouse Power Corporation Mixed powder deposition of components for wear, erosion and abrasion resistant applications
EP1743957A1 (en) * 2005-07-14 2007-01-17 Sulzer Metco (US) Inc. Process for treating the tip of a turbine blade and turbine blade treated by such a process

Also Published As

Publication number Publication date
KR20100018500A (en) 2010-02-17
US20100173094A1 (en) 2010-07-08
JP2010526232A (en) 2010-07-29
JP4910096B2 (en) 2012-04-04
EP2171124A1 (en) 2010-04-07
KR101372342B1 (en) 2014-03-12
CA2679517A1 (en) 2008-11-13
US9322100B2 (en) 2016-04-26
EP2171124B1 (en) 2011-09-14
WO2008135803A1 (en) 2008-11-13
CA2679517C (en) 2014-02-11

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